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Overview

MR-106L 22N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.59 kg, with a specific impulse of 228 to 235 sec and a thrust of 10 to 34 N (steady state).

Properties

Overview

Name
MR-106L 22N
Supplier
L3Harris Aerojet Rocketdyne
Type
Other
Flight proven
Yes

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